LTD LO-120S

{{Short description|German ultralight aircraft}}

{{Use dmy dates|date=January 2022}}

{{Use British English|date=January 2022}}

{{Infobox aircraft begin

| name=LO-120S

| image=

| caption=

}}{{Infobox aircraft type

| type=Ultralight aircraft and motor glider

| national origin=Germany

| manufacturer=Logistik-Technik

| designer=

| first flight=

| introduced=

| retired=

| status=In production (2011)

| primary user=

| more users=

| produced=

| number built=

| developed from= LO 120 S

| variants with their own articles=

}}

The LTD LO-120 is a German ultralight aircraft, produced by Logistik-Technik, of Baindt and based on the earlier LO 120 S produced by LO-Fluggerrätebau. The aircraft is supplied as a kit for amateur construction or as a complete ready-to-fly-aircraft.Bayerl, Robby; Martin Berkemeier; et al: World Directory of Leisure Aviation 2011-12, page 64. WDLA UK, Lancaster UK, 2011. ISSN 1368-485X

Design and development

The LO-120 was designed to comply with the Fédération Aéronautique Internationale microlight rules. It features a cantilever high-wing, a two-seats-in-tandem open cockpit with a small windshield, fixed tricycle landing gear and a single engine in pusher configuration.

The aircraft is made from wood, with its flying surfaces covered in doped aircraft fabric. Its {{convert|15.5|m|ft|1|abbr=on}} span soaring wing has an area of {{convert|16|m2|sqft|abbr=on}} and can be quickly swapped for an alternate, reduced span microlight touring wing that increases cruising speed. The tail is an inverted V-tail mounted to twin booms. The standard engine is the {{convert|40|hp|kW|0|abbr=on}} Rotax 447 two-stroke powerplant.

Cockpit access is via a sliding fairing.

Specifications (LO-120S)

{{Aircraft specs

|ref=Bayerl

|prime units?=met

|genhide=

|crew=one

|capacity=one passenger

|length m=

|length ft=

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|span m=15.5

|span ft=

|span in=

|span note=(soaring wing)

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|wing area sqm=16

|wing area sqft=

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|airfoil=

|empty weight kg=220

|empty weight lb=

|empty weight note=

|gross weight kg=400

|gross weight lb=

|gross weight note=

|fuel capacity={{convert|70|L}}

|more general=

|eng1 number=1

|eng1 name=Rotax 447

|eng1 type=twin cylinder, air-cooled, two stroke aircraft engine

|eng1 kw=30

|eng1 hp=

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|perfhide=

|max speed kmh=150

|max speed mph=

|max speed kts=

|max speed note=

|cruise speed kmh=130

|cruise speed mph=

|cruise speed kts=

|cruise speed note=

|stall speed kmh=60

|stall speed mph=

|stall speed kts=

|stall speed note=

|never exceed speed kmh=

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|range km=

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|ceiling m=

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|climb rate ms=3.5

|climb rate ftmin=

|climb rate note=

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|wing loading kg/m2=25

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}}

References